Ethiopian airliner down in Africa
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There is this volumous clanking noise going on, as the huge great Titanic trim wheel (taken from the Ju-52) winds its way around. And the controls will need a great deal of pulling for normal flight (something like 50 to 60 kg of force), which is pretty much uncontrollable.
You do not get a continuous running of the trim wheel like in a trim runaway, so probably not so easy to understand, at least not as easy as some posters imply.

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"200hrs [total] and already in the cockpit of a big plane" is another question, but in some parts of the world it is a reality. (I.e. Russia.)

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Couple of things,
If i have read correctly there is come kind of update Boeing is working on in regards to the MCAS system following JT610, what is this update meant to actually do and what is it meant to prevent?
What is the failure rate of an AOA sensor, lets say this crash is related to MCAS, 2 aircraft which are less than 4 months old to both have failures of the same sensor regardless of MCAS seems very odd to me?
If i have read correctly there is come kind of update Boeing is working on in regards to the MCAS system following JT610, what is this update meant to actually do and what is it meant to prevent?
What is the failure rate of an AOA sensor, lets say this crash is related to MCAS, 2 aircraft which are less than 4 months old to both have failures of the same sensor regardless of MCAS seems very odd to me?


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Bird strike on non redundant single AOA sensor doesn't allow much time to negotiate.


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I think the FAA is one of the only ones to require ATP for FO's.

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It takes just one bird to lose an AOA sensor - we had that happen just a couple of weeks ago on one of our NGs.
Last edited by xetroV; 11th Mar 2019 at 10:17.

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You could expect those kind of comments from the average (non frequent flyer) passenger, not from somebody who claims to be a former airline pilot. THERE IS NO PROVEN EVIDENCE SO FAR that the Ethiopian accident has been caused by a technical issue that, despite having been WELL MANAGED (that is another very important point) by the flight crew, ended up in a disaster anyway.
Only 350 of these birds have been delivered. Two have crashed, with what appears to be superficial commonalities, in less than 6 months.
I wouldn't necessarily avoid travelling on the type, but I wouldn't be critical of somebody who does.

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MCAS only operates in very high (or faulty) AoA, which would probably prevent the AP from being engaged.

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FYI. My employer has just sent out a message instructing its employees to avoid flying on 737 MAX 8 aircraft. The company has no aviation expertise, but has dozens, maybe 100s, of employees in the air at any given moment. I doubt if this is backed by a genuine risk analysis - I wonder if it will actually push pax onto smaller and possibly less well managed airlines ? I am sure lots of other organisations are doing the same; I think all airlines will have no choice but to ground this aircraft.

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Ironic that members here who blame the MCAS system already are switching to A320s for their flights which also have the same type angle of attack sensors along with software to prevent a stall and have received faulty see also from sensors resulting in a fatal crash before the crew could respond. It was 10 years ago the A320 with 3 sensors had 2 freeze due to maintenance, the software selected those 2 to use neglecting the third working AOA sensor because it differed, put the plane into a stall preventing dive at an altitude from which the crew could not recover before plunging into the Med. darn Boeing copying AB.

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Just looking at a profile picture of the 737 - 8 Max, it strikes even the mildly interested, that those huge new engines are positioned almost completely foward and clear of the leading edge of the wing. That must shove the Centre of Gravity of the aircraft way in front of the leading edge of the wing. That's non-standard for a start in a passenger aircraft. Usually the C of G is positioned on or just foward of the centre of lift.
N.
N.

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I would like to note that Boeing appear have a suffered disproportionate number of crashes where their aircraft dived nose first into the ground:-
Even though spread over many years, it does appear to be pattern, notwithstanding the very different causes involved. I cannot remember any of the competing airliners having similar problems - Fokker, BAC, Convair, Sud Aviation, Airbus etc.
- 737-200, UAL flight 585 (rudder problem)
- 737-300, USAir flight 427 (rudder problem)
- 737-800 FlyDubai flight 981 (loss of control during go around. Wikipedia indicates stabilizer trimming was involved)
- 737 Max 8 Lion air flight 601 (suspected AOA/MCAS issue)
- 767 Atlas Air Flight 3591 (unknown problem)
- 737 Max 8 Ethiopian Airlines (unknown problem)
Even though spread over many years, it does appear to be pattern, notwithstanding the very different causes involved. I cannot remember any of the competing airliners having similar problems - Fokker, BAC, Convair, Sud Aviation, Airbus etc.

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It would be interesting to get an idea if anyone else has been having sensor and MCAS problems. We know that the Lion aircraft experienced issues over several days. It seems inconceivable that the Ethiopian aircraft could have experienced anything similar and it not be written up. There are however a number of similarities so far between the two 737 Max accidents. For example both were first flights of the day from the airline's home base. It is quite likely that a daily check would have been carried out by company maintenance personnel shortly before the flights (in the Lion case we know for sure). It is also quite possible the aircraft were powered down before the accident flights, which may or may not be relevant, but experience has taught me that odd gremlins can occur when powering up electronic systems. Both crews lost control shortly after takeoff and impacted terrain. We will find out pretty soon from the flight recorders what happened.
Should it turn out to be the same failure then this is going to be a huge problem for Boeing. I flew the NG for many years and it together with the 777 have had absolutely outstanding safety records and very successful production runs. To lose two brand new Max aircraft within such a short period of time will raise big issues for the program. I have to say that given the present uncertainty I would not go out of my way to fly on a 737 Max until things have been clarified.
Should it turn out to be the same failure then this is going to be a huge problem for Boeing. I flew the NG for many years and it together with the 777 have had absolutely outstanding safety records and very successful production runs. To lose two brand new Max aircraft within such a short period of time will raise big issues for the program. I have to say that given the present uncertainty I would not go out of my way to fly on a 737 Max until things have been clarified.

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Learned Contributors,
please excuse if this is considered thread drift. If this Ethiopian crash and the Indonesian previously covered on here are proved to be linked. Is
not it odd that out of the total number of B.738M departures since entry to service, no one has been subject to this upset and caught it without loss of life ? Especially since Indonesia as I expect all B.738 Max crews are looking out for a recurrence?
Your time and trouble much appreciated,
Be lucky
David
please excuse if this is considered thread drift. If this Ethiopian crash and the Indonesian previously covered on here are proved to be linked. Is
not it odd that out of the total number of B.738M departures since entry to service, no one has been subject to this upset and caught it without loss of life ? Especially since Indonesia as I expect all B.738 Max crews are looking out for a recurrence?
Your time and trouble much appreciated,
Be lucky
David

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For those fixated on the experience level of the first officer, have we stopped to think of the possibility that the information given out on his/her experience level may be false. So far the only official statement I have read or heard about the experience of the pilots is that of the captain which says he is a senior Captain who has been with Ethiopian for 9 years.
Lets think about this for a minute, 200 hours doesn’t making sense taking into consideration average time to qualify for a CPL, the average time for line training and to get checked out on line as a first officer or second officer at the airline or was this a line training flight with a training captain?
As is common knowledge and has always been said on here, having a low time pilot as a first officer straight out of flight school is not uncommon, this is practiced all over the world and so far without issues, lots of very experienced and very good captains today started that way, not every country has their aviation industry set up like the US to start off in the general aviation sector and work yourself up to the majors.
Lets think about this for a minute, 200 hours doesn’t making sense taking into consideration average time to qualify for a CPL, the average time for line training and to get checked out on line as a first officer or second officer at the airline or was this a line training flight with a training captain?
As is common knowledge and has always been said on here, having a low time pilot as a first officer straight out of flight school is not uncommon, this is practiced all over the world and so far without issues, lots of very experienced and very good captains today started that way, not every country has their aviation industry set up like the US to start off in the general aviation sector and work yourself up to the majors.

There is always a superman, who knws everything. But how many times have you operated these switches? I think I have touched them twice in 10 years. Still know which way they operate? And warnings going off all over the place; and the aircraft pitching up and down, possibly violently; and you only have 200 hours on type .... still know which way these switches operate...?
Silver
Runaway trim is a recall item. It doesn't take a superman to know the memory items it's a requirement of the job. Heaven forfend.
