Originally Posted by DaveReidUK
(Post 10415633)
It will likely position back to Luton shortly.
EASA has stopped all MAX flying from 1900Z One TUI MAX was circling Bologna at 1859z - ?? where to park the upcoming static display whilst en route with pax from Egypt to BRU ?? |
Political decission
It appears that air safety and airworthiness is a political decision in the end? When most of the western world has grounded the MAX, US is still arguing it's business as usual.
|
Originally Posted by rog747
(Post 10415647)
Do you think so Dave?
EASA has stopped all MAX flying from 1900Z |
Originally Posted by FCeng84
(Post 10415561)
1. First thing is pull the column to put in the between 5 to 8 degrees of airplane nose up elevator needed to offset the MCAS stabilizer increment.
2. Use manual pitch trim to re-establish trim to the point of not needing to hold column. 3. If stabilizer runs airplane nose down again, recognize it as inappropriate and arrest by using manual pitch trim to stop MCAS stabilizer motion and move stabilizer back to trimmed position. (No need to sit idly by and watch 10 seconds of stabilizer motion taking you away from trim go in when you have determined that is not appropriate.) 4. Call for PNF to toggle stabilizer cutout switches and discuss managing pitch trim via manual trim wheel for the balance of this flight. 5. Make sure that this event is squawked in a manner that assures: - The source of the errant stabilizer motion is identified and corrected prior to the next flight - The next crew to fly this bird knows full well what was encountered on this flight and what was done to work around it. Sat typing at a keyboard it appears obvious. All pilots will be able to tell you the memory items. |
Pilot error
"Pilot induced oscillation" and "some pilots are not as well trained as pilots in US": https://video.foxnews.com/v/60130558...#sp=show-clips
|
IF (of course it's still a big IF) a faulty AOA sensor input is at fault again here feeding MCAS invalid AOA position, a person might want to look into the recent Quality assurance and manufacturing of those AOA probes. I would assume the Lion Air and ET Max's are not too far off of each other, which may have a similar batch of AOA probes.
I agree that the simple and appropriate fix to the system would be to have to see 2 valid AOA inputs for a stall or near stall position. It's hard to believe they would engineer such a critical system with only one AOA input required. |
Originally Posted by procede
(Post 10412067)
Another AoA / stall recovery / horizontal stabilizer autotrim problem?
|
Originally Posted by DaveReidUK
(Post 10415650)
Neither the CAA nor the EASA restrictions preclude a ferry/positioning flight back to base.
|
Remember , stick pushers will only work if the elevators are big enough. The whole issue is that they're not. Hence the MCAS inputs a change to the angle of the whole tailplane. The whole back end should have had a redesign years ago, and also any critical AoA detectors should be triplicated (not just two).
|
Originally Posted by oldoberon
(Post 10414891)
my quote tells you LANCS THINKS it is in the Lion Air thread, which is why I started my post off with IF IT IS TRUE..
Oldeberon |
In my experience, I was under the impression that if automation was likely to be causing a problem, you reduce the level of automation. It appears from what I’m reading, that it is when the autopilot is disconnected that the MCAS becomes armed. Personally I think this goes against the philosophy most pilots understand, whether or not it is applicable to this accident. I’m only Boeing/Gulfstream btw. |
12MAR 20:35
European Countries applying B737-8 MAX and B737-9 MAX Airspace Restrictions AO's are informed that below mentioned European States are not accepting entry into their airspace of any airline operating their flight with B737-8 MAX and B737-9 MAXtype of aircraft. Please find the list of valid NOTAMs below : NOTAM B0386/19 refers for UK/Northern Ireland ACC. NOTAM B0235/19 for Irish ACC. NOTAM A0612/19 for Vienna ACC. NOTAM F0373/19 for all French ACCs. NOTAM A0822/19 for Belgian ACC. NOTAM A0177/19 for all German ACCs. NOTAM C0206/19 refers for Warsaw ACC. NOTAM B1615/19 for Canary ACC. NOTAM A1673/19 for all Italian ACCs. NOTAM A0333/19 for Amsterdam ACC. NOTAM B1614/19 for all Spanish ACCs. NOTAM A0499/19 for Vilnius ACC. NOTAM A0123/19 for Swiss ACCs. NOTAM A0253/19 for Slovenian ACC. NOTAM A0355/19 for Cyprus ACC. NOTAM G0036/19 for Tbilisi ACC. Please note that B737 800 is not affected by this. NMOC Brussels |
Originally Posted by FCeng84
(Post 10415636)
The 737 is not a fly-by-wire airplane and thus does not have an augmented elevator command when flying manually.
.
Originally Posted by FCeng84
(Post 10415636)
As mentioned via earlier posts in this thread, modifications to MCAS have been developed and will be out to the fleet this spring to improve MCAS safety. One of the key factors is removing the assumption that the crew, having activated manual trim, will provide complete manual trim to zero column force.
Silver |
The last B38M Smartwings revenue flight QS1201/TVS1201 has been caught off-guard over the Black Sea. Flying circles, nowhere to land...
|
Originally Posted by Albino
(Post 10415655)
You may well believe it's that simple. There are plenty of distractions in the real world from ATC, terrain, weather/turbulence etc. That's before the stick shaker activates and the autopilot disconnects. Whilst you are trying to work out why that has happened (because it could be a variety of reasons) and fly the aircraft (including trimming), the aircraft is working against you. And this aircraft trims automatically on every departure, often against you.
Sat typing at a keyboard it appears obvious. All pilots will be able to tell you the memory items. Two important things to keep in mind with MCAS: - It will not activate with flaps down and thus will not be active on climbout until the flaps are retracted. If there is a gross AOA error (as on Lion Air) the stick shaker will be firing as soon as you get into the air. With this scenario you get a heads up that something is wrong with AOA before experiencing MCAS. - If you continue to fly the airplane with the column and followup with pilot pitch trim to drive the column forces to zero you will have plenty of pitch control authority to fly your intended path. |
The last B38M Smartwings revenue flight QS1201/TVS1201 has been caught off-guard over the Black Sea. Flying circles, nowhere to land.. QS4160 SID-PRG is taking a very unusual routing, currently heading in the direction of Malta. |
Originally Posted by adr
(Post 10415685)
I've not seen the EASA notice, but can you help me to understand how the CAA one permits a positioning flight? Does "must not be flown" (2.1a, 2.1b) mean something different to the interpretation I'm giving it?
The CAA's initial announcement of the restriction on its website and its Twitter feed (both still up) say specifically "[we have] issued instructions to stop any commercial passenger flights from any operator arriving, departing or overflying UK airspace." See UK Civil Aviation Authority statement. I agree that the Safety Directive (which I hadn't seen) appears not to allow any flights at all (even though the EASA Emergency AD does). I guess the proof of the pudding will be whether that TUI Max 8 does in fact position back to the UK. |
Originally Posted by virginblue
(Post 10415731)
Not really. It departed Dubai hours ago and surely has not been caught off guard when approaching EU airspace.
QS4160 SID-PRG is taking a very unusual routing, currently heading in the direction of Malta. UPD. The poor guys are still circling closer to Turkish coast. |
Originally Posted by silverstrata
(Post 10415718)
What Boeing REALLY needs to do is have multiple inputs to the MCAS, so it is not reliant on a single AoA sensor. At the very least MCAS needs to drop out if it senses a mismatch between the AoA sensors, and just flag an error-fault. The last thing MCAS should be doing is activating its protocols, when it must know that the AoA sensors are in disagreement. Silver How can an aircraft's certification be reliant on one single AoA vane always functioning correctly? I know it's been brought up about Airbus having 3 sources, but if you designed it correctly, you could have 100 mini AoA sensors for this function, and only let the software control flight surfaces when at least say 60 are in agreement! The software isn't the problem, the problem is the fact that the software relies on a single data source that isn't verified. Others have commented about the AoA being cross-checked against ASI etc. before making control inputs, that would be a good start. AND... if you're going to throw in different functions and automated controls onto an aircraft, please have the decency to let the professional crew know what they are and how they work first, just in case they do something they shouldn't! P.S. How many backdoor, certification reliant, automated controls are there that can function when AP is off? Or is MCAS the the only one so far? |
Originally Posted by hans brinker
(Post 10415729)
MCAS is because of the aerodynamic effect of the bigger engines, they create "lift" at high AOA, leading to even higher AOA. Nothing to do with the engine power.
|
All times are GMT. The time now is 22:34. |
Copyright © 2024 MH Sub I, LLC dba Internet Brands. All rights reserved. Use of this site indicates your consent to the Terms of Use.