European and American regulators have gone over it with a fine tooth comb at this point and allow it to fly. There is always gonna be people that will say the plane shouldn't fly. Arguably the amount of attention this plane has gotten will probably make it one of the safest in the industry going forward.
>Travis is unequivocal in his assessment of the Boeing 737 MAX. “It’s a faulty airframe. You’ve got to fix the airframe [and] you can’t fix the airframe without moving the engines” back and away from their current position.
>The root problem with the engine-forward design is “once this thing pitches up, it wants to keep pitching up,” said Travis. “That’s a big no-no,” he continued, because pitch-up on an aircraft increases angle of attack.
https://www.eetimes.com/software-wont-fix-boeings-faulty-air...
"Gregory Travis, a veteran software engineer and experienced, instrument-rated pilot who has flown aircraft simulators as large as the Boeing 757"
I know a few veteran software engineers that are instrument-rated and frankly I'm not sure I would listen to any of them over the FAA or aeronautical engineers. Probably good for some perspective, but not exactly a great source for determining if an airplane is "aerodynamically flawed by design".
"who has flown aircraft simulators as large as the Boeing 757"
Talk about a big aircraft simulator, those that I know are the size of a car, not of a 757 (jk)
He's somewhat right on other details, but that doesn't make his assessment of the aerodynamic issues correct.
Aircraft are designed to not let that happen in an uncontrolled fashion. Software has been used to do this since the advent of computers in airplanes
Maybe we should also start boycotting A320neo's too
https://www.flightglobal.com/programmes/a320neo-also-potenti...
Insufficiently tested and documented? Sure. Bad UI/UX? Most definitely. Irredeemable 'because of aerodynamics' according to some private pilot that flew a 737 once in sim? Absolutely not.
(Student Pilot and Mechanical Engineer here)
But yes. MCAS was put in place due to concerns over aero. If that was just to avoid the need for extra pilot training then it should have been scrapped since new training will be required now anyway. But since great effort has been made to fix MCAS we can conclude that the root problem is aerodynamic.
Can aerodynamic issues be compensated for with software? Sure. I need to read up on the final hardware/software/instruction solution before passing Judgement.
The big flaws are in the software, not in the hardware. So stop focusing on that.
Would the software even be necessary if the airframe was better designed?
[0] https://en.wikipedia.org/wiki/McDonnell_Douglas_MD-11#Accide...
He said that was the the reason airlines switched to using them as cargo planes.
I realise this is just an anecdote, though.
The MD-11 has been certified for air transport since it was introduced, was flying in revenue service until 2014, and as far as I know, that certification has never been revoked.
The 737 Max has different yoke force during pitch-up than predecessor 737 models, such that at higher angles of attack it does not natively require increasing yoke force to continue to pitch up. That doesn't mean it would pitch up uncontrollably. MCAS was designed to provide pitch-down force in these high-AoA cases so that yoke forces would be equivalent to 737 NG models and minimal training would be necessary to fly both.
And while military planes are quite different from commercial planes, many (most at this point?) military jets are aerodynamically unstable.
Longitudinal stability is something of a special case, in that essentially all swept-wing aircraft are vulnerable to "Dutch roll" instability and are generally fitted with yaw dampers. Since such stabilizers are, practically-speaking, omnipresent, regulators are OK with using them in what is now a well-understood domain. While it can be unpleasant, all of these aircraft can be flown with a failed yaw damper - notably the 707 family has a particular proclivity for yaw instability, and while almost all civilian users opted for the yaw damper, the largest fleet user, the USAF, did not fit their KC-135s with dampers until well into their service life.
For good reason, pitch instability is a much more serious issue, and there has been very little interest in trying to bring to market a transport aircraft that required active pitch stabilization. Many, if not all, modern clean-sheet airliner designs are fly-by-wire due the the safety, performance, and efficiency improvements to be had, but they are all safely flyable in an "alternate law" (or equivalent) fallback mode.
Combat aircraft, generally speaking, aren't certified aircraft (they have no need be), for good reason - if you're flying a modern fighter and the FBW computers die on you, it's over, you eject. Understandably, that's not an option in a transport aircraft.
I think the Max will crash again. Excuse me, the 737-8 will crash again.
I mean all else being equal (Two planes to London leaving at almost exactly the same time and exactly the same cost) then perhaps I'd prefer the A32X. But the point is all else isn't equal. It becomes a matter of how many hundred you want to spend to fly the Airbus. Or how many hours you want to spend at the airport waiting for the non-Max flight. And I'll happily take the MAX if it saves me 30 minutes or $20. And I'll take my family along too without hesitation.
The whole thing has been badly handled. The FAA/EU agencies should have declared at the very outset that airlines will need to bear the cost of retraining the pilots who will be flying this. It was the attraction of not having to retrain pilots that was the biggest incentive for Boeing to pull the shortcuts they did. At a bare minimum the aviation agencies should have pulled that benefit away.
AA seems to show "7M8-Boeing 737MAX 8" though.
See https://onemileatatime.com/american-737-max-flights/ and https://onemileatatime.com/boeing-737-8/
ADDED: And I'm guessing things are more fluid than usual in the current situation.