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Old 06-24-2019, 02:40 PM
  #3611  
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Originally Posted by TED74
... and max reverse on a Maddog can overtemp the motors and contribute to runway departure on landing.

Let's not design out all the issues...I want to earn the ridiculous compensation I expect in our next contract!
MCAS: Keeping pilotless airplanes at bay since 2019

Vs

Airbus A350: Tempting the world to go pilotless since 2013

Last edited by forgot to bid; 06-24-2019 at 03:05 PM.
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Old 06-24-2019, 02:58 PM
  #3612  
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Originally Posted by Xray678
Nothing wrong with the airplane? The engine is mounted in such a way that at high angles of attack, the airflow over the nacelles causes the nose to go even higher.

Even if you don’t consider that to be something wrong with the airplane, I have zero confidence Boeing with completely fix MCAS until there is another accident.
Interesting. The A330-900 has the engines moved up and forward for clearance creating a greater nose pitchup on thrust application. Airbus fixed it with software.
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Old 06-24-2019, 03:03 PM
  #3613  
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Originally Posted by sailingfun
Interesting. The A330-900 has the engines moved up and forward for clearance creating a greater nose pitchup on thrust application. Airbus fixed it with software.
100% FBW gets a pass.

I mean both ailerons can go up in flight on an Airbus if it wants them too... FBW gonna FBW.
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Old 06-24-2019, 03:21 PM
  #3614  
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Originally Posted by Xray678
Nothing wrong with the airplane? The engine is mounted in such a way that at high angles of attack, the airflow over the nacelles causes the nose to go even higher.

Even if you don’t consider that to be something wrong with the airplane, I have zero confidence Boeing with completely fix MCAS until there is another accident.
From what I've read the additional nose up (only at certain AoA, weight and thrust conditions) was so slight compared to the NG that only the sharpest test pilots could tell it was barely a thing. But since it technically was, and they wanted to avoid what would have became one more sim lesson, they backward engineered that asinine system instead to roll in full nose down trim (um, WTAF?) for either that rare and still relatively benign very slight additional pitch up moment or a single inop sensor.

From what I've seen looking into this, there was nothing wrong with the plane and the mass media talking point that it pitched up and therefore needed that MCAS system was massively exagerated and faithfully repeated. The best, most thorough articles and videos I've seen on it contradict the pop culture narrative that the engine mounting issue would somehow cause an uncontrollable tail stand that would send it into a flat spin out to sea. Far from it. Instead since it felt slightly different, it would trigger a single differences sim and there was a lot of pressure all around to avoid that.

In any case, there should never, ever, be a system that rolls in full nose down trim with a wheel you have to turn a billion times to undo with load forces too strong to even do that, all for a problem that reportedly was very minor to begin with.

The MAX will be fixed and thousands of them will fly safely for decades to come.
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Old 06-24-2019, 03:48 PM
  #3615  
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Originally Posted by gloopy

In any case, there should never, ever, be a system that rolls in full nose down trim with a wheel you have to turn a billion times to undo with load forces too strong to even do that, all for a problem that reportedly was very minor to begin with.
... particularly when the impetus can be a single malfunctioning probe?!

That horrendous risk analysis makes me wonder what other gremlins live in this and other Boeing products. Hopefully a thorough internal review is underway and processes going forward will be measurably different.
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Old 06-24-2019, 04:23 PM
  #3616  
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Originally Posted by Xray678
I do think it is something wrong with the airplane, given that Boeing wanted commonality with previous 737s. It drove the MCAS system, which previous generations didn’t have. What if that system is inop. You can’t MEL it. If it fails inflight, now you have an airplane that doesn’t handle as advertised and pilots are not trained to understand. Yes that’s something wrong with the airplane.

Besides, I don’t buy that MCAS was simply to make it handle like previous 737s. I don’t believe, based on some articles I have read, that the MAX complies with FAR part 25 regarding stall characteristics or longitudinal stability without MCAS. Further, I don’t believe Boeing would have spent the money and time to add MCAS if the handling characteristics of the MAX were inherently safe.
After wading through all the Baghdad Bobisms, I think you're exactly correct.
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Old 06-24-2019, 04:23 PM
  #3617  
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Originally Posted by forgot to bid
100% FBW gets a pass.

I mean both ailerons can go up in flight on an Airbus if it wants them too... FBW gonna FBW.
Yup. It doesn't need a redneck patch to an antiquated flight control system.
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Old 06-24-2019, 04:37 PM
  #3618  
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Originally Posted by 80ktsClamp
After wading through all the Baghdad Bobisms, I think you're exactly correct.
I mean if it was a simple fix it'd be flying by now, right?

Imho I think they're trying to figure out how to do a major fix without admitting it needed a major fix.

So they're probably trying to find any MD-90 and 11 engineers, theyll know what to do.
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Old 06-24-2019, 04:55 PM
  #3619  
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Originally Posted by gloopy
All that, plus if its already a very small market to begin with, there really won't be much room in doubling capacity. Or 3X/4X if others do it.

And I find it very hard to believe the A318/319 can do it but the 737-700 and 757 can't.

The hype around LCY and the A220 has managed to exceed even the most exuberant ULCC dreams of self printing money by flying to ultra saturated, low yield, loss leader Hawaiian markets.

The 787 was supposed to not just do the occasional niche route (which I'm sure it does a few) but it was supposed to disrupt the entire industry like a Model T among horses and eliminate the hub and spoke model by darkening the skies with "long and thin" fantasy routes. Its done no such thing and it never will.

Yet now here come the pundits claiming the A220 is some "game changer" nothing can compete with (and the 321XLR now too I guess LOL).
The big cert issue at LCY is the requirement to fly a 5.5⁰ glide slope which means prove the plane can fly a 7.5⁰ slope to handle any poor technique, etc. Most planes go down the slope with some or all of the boards extended and even then some can’t do it and maintain anti-icing protection.

GF
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Old 06-24-2019, 05:33 PM
  #3620  
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Originally Posted by galaxy flyer
prove the plane can fly a 7.5⁰ slope to handle any poor technique, etc.

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Also known as the MCO 18R Visual
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