Go Back  Airline Pilot Central Forums > Pilot Lounge > Safety
Ethiopian 737 MAX 8 crash >

Ethiopian 737 MAX 8 crash

Search
Notices
Safety Accidents, suggestions on improving safety, etc

Ethiopian 737 MAX 8 crash

Thread Tools
 
Search this Thread
 
Old 03-19-2019, 06:29 AM
  #321  
Prime Minister/Moderator
 
rickair7777's Avatar
 
Joined APC: Jan 2006
Position: Engines Turn Or People Swim
Posts: 39,244
Default

Originally Posted by nfnsquared View Post

1. Yes, something like that. I assume all sensors feed to a data bus of some sort? As I understand it, each of the 2 FCCs gets data from a single AOA sensor, not both. Wondering if the fix is for the active FCC to read from both AOAs or for the active FCC interact with the non-active FCC to compare AOA inputs?


2. Already done, but I know what you mean...


3. I would assume it could be done fairly quickly, assuming a central data bus or an easy interconnect between data busses which would make the fix purely a programming fix? That may be the fix that Boeing was about to push?



I assume a disable switch would just be a logic input to tell the active FCC to quit the MCAS routine?
Probably, since they already HAVE hardwired trim cutout switches.

Also probably some sort of cockpit indication that MCAS is functioning. Probably also a limit on repetitive MCAS operations, so it doesn't keep repeating the process indefinitely in response to bad data. It doesn't move the trim that far or that fast, the problem is when it keeps doing it over and over again intermittently.
rickair7777 is offline  
Old 03-19-2019, 06:38 AM
  #322  
Gets Weekends Off
 
Joined APC: Mar 2014
Posts: 281
Default

Originally Posted by Fdxlag2 View Post
Thus the fix. The problem wasn’t the system is bad. The problem was a singled failed AOA indicator could activate it. The fix is it will take two to activate it. If both AOA indicators say you are stalled, you are probably stalled.
I probably did not make myself clear and apologize. What kind of failure would it take for the system not to be blocked out when the flaps are deployed? Would the failure of a (single?) flap position sensor allow for the system to engage with the flaps deployed when both AOA sensors sensed a high AOA at lift-off or landing? Does the MAX have or does it need two flap position sensors in addition to the other fix?
F4E Mx is offline  
Old 03-19-2019, 06:39 AM
  #323  
Prime Minister/Moderator
 
rickair7777's Avatar
 
Joined APC: Jan 2006
Position: Engines Turn Or People Swim
Posts: 39,244
Default

Originally Posted by BoilerUP View Post
Boeing may have destroyed the tooling, but I’d bet they still have all the engineering documents for them...
I'm sure they do since they still support the plane. But that's not the same as being able to build it, they would essentially have to start from scratch, minus whatever old-timer 757 vets are still employed there (or could be enticed out of retirement). They might even still have the tooling stored away, in case they had to build a major structural part for some reason.

Boeing and Airbus are good at what they do, but their ecosystems are not designed or evolved to restart long-dead production lines. Much harder than you might think.

It would be an economically ludicrous proposition anyway. They are not even sure they can make a business case for a NEW design NMA...
rickair7777 is offline  
Old 03-19-2019, 07:21 AM
  #324  
Gets Weekends Off
 
Joined APC: Nov 2016
Posts: 936
Default

Originally Posted by F4E Mx View Post
I probably did not make myself clear and apologize. What kind of failure would it take for the system not to be blocked out when the flaps are deployed? Would the failure of a (single?) flap position sensor allow for the system to engage with the flaps deployed when both AOA sensors sensed a high AOA at lift-off or landing? Does the MAX have or does it need two flap position sensors in addition to the other fix?
Beats me. One single actuation of the MCAS is not going to make an aircraft uncontrollable. The problem was there were multiple cumlative activations of nose down trim. That too has been addressed. In your scenario, Boeing has a disagree logic. If the flap handle and any the trailing/leading edge devices aren’t in agreement you are notified. They could easily make sure MCAS does not engage unless the handle and the devices agree flaps are up.

They are not stupid, but they did take shortcuts to get the max approved. It will cost them plenty.
Fdxlag2 is offline  
Old 03-19-2019, 09:44 AM
  #325  
Gets Weekends Off
 
Joined APC: Jan 2006
Posts: 222
Default

Originally Posted by Fdxlag2 View Post
Beats me. One single actuation of the MCAS is not going to make an aircraft uncontrollable. The problem was there were multiple cumlative activations of nose down trim.
The problem is, the system was designed to kick in multiple times. In not, then in an actual stall, with a nose up trim, the system will activate, you will click the thumb switch to relieve the perceived pressure which will kill the MCAS. In that configuration with substantial nose up trim and in a stall you may not recover unless you apply nose down trim.
sgrd0q is offline  
Old 03-19-2019, 09:46 AM
  #326  
Gets Weekends Off
 
Joined APC: Aug 2013
Posts: 2,159
Default

Originally Posted by BoilerUP View Post
Boeing may have destroyed the tooling, but I’d bet they still have all the engineering documents for them...

Not sure on this. but didn't Boeing re start the 767 line so they could build the USAF some tankers?

I would much rather be flying around in an updated, and quite capable, quite tested, and very proven B 757 then trying to put the round peg in the square hole from a design perspective with these new Maxxed out 737's.

Boeing should simply say this: The Mission of the B737 is X. The mission of the B 757 is Y. Which jet do you want? We can and will build what you need.

I guess we are being forced to wait for the 797 to get the replacement for the 757?
baseball is offline  
Old 03-19-2019, 09:48 AM
  #327  
Gets Weekends Off
 
Joined APC: Nov 2016
Posts: 936
Default

Originally Posted by baseball View Post
Not sure on this. but didn't Boeing re start the 767 line so they could build the USAF some tankers?

I would much rather be flying around in an updated, and quite capable, quite tested, and very proven B 757 then trying to put the round peg in the square hole from a design perspective with these new Maxxed out 737's.

Boeing should simply say this: The Mission of the B737 is X. The mission of the B 757 is Y. Which jet do you want? We can and will build what you need.

I guess we are being forced to wait for the 797 to get the replacement for the 757?
Nope Boeing sold FDX 76s at a discount to keep the line open.
Fdxlag2 is offline  
Old 03-19-2019, 09:54 AM
  #328  
Gets Weekends Off
 
Joined APC: Nov 2016
Posts: 936
Default

Originally Posted by sgrd0q View Post
The problem is, the system was designed to kick in multiple times. In not, then in an actual stall, with a nose up trim, the system will activate, you will click the thumb switch to relieve the perceived pressure which will kill the MCAS. In that configuration with substantial nose up trim and in a stall you may not recover unless you apply nose down trim.
I think you will find it is no longer designed to kick in multiple times before the max ever flys again. At least that is what The Seattle Times says Boeing says. It was never supposed to be able to move the trim that much. But the designers failed.
Fdxlag2 is offline  
Old 03-19-2019, 04:47 PM
  #329  
Gets Weekends Off
 
pangolin's Avatar
 
Joined APC: Jul 2017
Position: CRJ9 CA
Posts: 4,083
Default

Originally Posted by Peacock View Post
MCAS doesn’t work with the autopilot on. The whole point is to avoid pitching nose up at high AoA when hand flying. Also, if this is the same thing as the Lion Air incident autopilot was probably not an option.

The flight the night before the Lion Ait crash had stick shaker start at rotation, with associated stall warnings which leads one to believe the airspeed is unreliable. Once they climbed away and raised the flaps, MCAS started trimming nose down. The crew the night before used the stab trim cutout switches and landed.
First I’m not saying this happened. But this could happen.

Climb out normal. Autopilot on. AOA sensor fail. Airspeed disagree. Autopilot will disconnect. That situation could be handled perfectly by keeping everything the same. Same pitch same power. You are now hand flying. Now enter MCAS. This complicates things and can lead - even at first application - to pitch oscillations.

And the accident sequence. It’s not one thing that will get you.
pangolin is offline  
Old 03-19-2019, 04:55 PM
  #330  
In a land of unicorns
 
Joined APC: Apr 2014
Position: Whale FO
Posts: 6,461
Default

Originally Posted by rickair7777 View Post
Maybe. It's frankly also realistic to assume that US pilots can handle this sort of thing better. Maybe not all regional crews, but anyone flying a MAX in the US should have the experience and skill.
Would this apply to 767 crews too?
dera is offline  
Related Topics
Thread
Thread Starter
Forum
Replies
Last Post
vagabond
Foreign
10
10-10-2013 04:49 AM
ToiletDuck
Safety
5
08-08-2012 09:04 PM
vagabond
Hangar Talk
2
05-05-2007 06:23 PM
LAfrequentflyer
Hangar Talk
1
09-07-2005 11:34 AM

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are On
Pingbacks are On
Refbacks are On



Your Privacy Choices