That's the only people in the media with an agenda? You don't think that Boeing, SWA and American Airlines PR machine is cranking full blast to get articles out there in the media saying how safe the plane is, the solution was just a simple procedure that every pilot is trained on, every pilot we put in the simulator was able to land safely? You think media agenda only goes one way? You're smarter than that.
If I was Boeing, I would have at least:
- Disclosed that the actual amount of stabiziler travel available to the MCAS was 2.5 degrees per activation instead of the submitted .6 degrees.
- I would have correctly classified this system as a critical safety system and required at least two sensor inputs to avoid erroneous activation instead of one sole input.
- I would have included MCAS system information in the Pilot's Systems Manuals.
- I would have allowed the stabilizer trim brake system to stop trim movement opposite to pilot elevator input.
But, more to my point. (Emphasis below all mine.)
In all my previous posts, I haven't been trying to exonerate the crew from any wrong doing. Maybe they were inexperienced (it seems the case with Ethiopian FO). Maybe they screwed up. But, in my mind they were faced with a lot tougher problem I've ever been trained for. My opinion... this was not a simple runaway stab trim. Not by any stretch of the imagination.
You can start with the fact everyone who has said they trained for a runaway stab trim failure in the simulator has had the advantage of a trim brake that stops the trim from running as soon as pressure is applied to the yoke opposite to the trim. That right there should stop the conversation. The trim never really "runs away." It at most goes a fraction of a unit before the brake stops it, allowing time for troubleshooting the problem. This list can go on and one how this MCAS activation differs from the runaway trim that we are trained for.
I had a whole post thought out trying to explain again how this wasn't just a run-of-the-mill stab trim runaway, but then I read a post on Facebook made by a 737 pilot and it summed up exactly what I was going to type.
Boeing (and many posters) say "Hey, it's just a trim runaway. Do the drill and all is good." But this is not the simple trim runaway that the QRH contemplates. It starts with a stall warning stick shaker shortly after lift off. Close to the ground this will, and should consume both pilots undivided attention. After a number of seconds they realise that the airplane hasn't stalled and they start figuring out that they may have an airspeed and/or AOA problem.
This is a second problem to deal with on top of the first. And they can't shut the &%$#@ stick shaker off once they realise that it may be spurious.
(Sluggo63: For anyone who doesn't know how distracting the stick shaker can be) The PM will be frantically scanning the panel to try and find some clue what is going on. And this whole time, among the din of the stick shaker, crews concern for the airplanes flight path, and the confusing instrument indications, MCAS has been intermittently dialing in nose down trim. Not steadily, in a calm cockpit at altitude like the QRH contemplates.
But intermittently in the background of chaos, noise, and confusion. At some point, well past when it would have been timely, the task saturated PF realizes that the trim is working against him/her and the stab cutout switches get turned off. (hopefully)But the ****show isn't over. Because of everything else going on, this took too long and the airplane is way out of trim. The Lion Air crew reportedly had 60 KG of back pressure on the yoke. Close to the ground, and relying on the lifting component of the underslung engines to help keep the nose up, the crew do not dare reduce power. Now the crew needs to manually trim the airplane, but the airplane is way, way off its trim speed. The B737 QRH makes reference to the large forces
that may be required to break free a servo clutch:
"3 If needed:Use force to cause the disconnect clutch to disengage. Approximately 1/2 turn of the stabilizer trim wheel may be needed.Note:A maximum two-pilot effort on the trim wheels will not cause a cable or system failure."Worse, the "Manual Stabilizer Trim" section of the Boeing FCTM talks about the air loads on a grossly out of trim stab requiring a speed change to reduce the force required to manually trim:
"Excessive air loads on the stabilizer may require effort by both pilots to correct mis-trim. In extreme cases it may be necessary to aerodynamically relieve the air loads to allow manual trimming. Accelerate or decelerate towards the in-trim speed while attempting to trim manually." Sweet Jesus how did this thing get certified?
A guy (or petite gal) has a 60 KG+ force on the yoke trying to stop the airplane from impaling itself into the hard ground just a few thousand feet below, and now he/she has to brute force trim the airplane as well, requiring involved coordination with the PM. Still with all the stick shakers, aural warnings, goofy instrument readings, and whatever else is happening to distract the crew and making communication almost impossible. It is not hard to see how quickly it becomes overwhelming.In addition to a fix for the airplane, if they keep the MCAS system (instead of designing a whole new wing or tail for the airplane), they will have to train the pilots who fly it to deal with its failure.
Right now, there is not a single Max pilot in the world who has been trained for this failure because - there isn't a single simulator in the world that can replicate it. But when they do, all those pilots that claimed "it's just a trim runaway" are going to have a very eye opening simulator session."
My only disagreement with the above is in the third paragraph. I don't know how far out of trim the plane was. At least in Lion Air, it looked like the Captain was doing a fairly descent job reversing the trim that the MCAS put in. Once he handed it over to the FO, it seems like his trimming was less effective than the Captain's.
About that new training. This is a from a buddy of mine who is a 737 Captain for one of the US airlines affected by the grounding regarding the AD and the training and information they received on MCAS. He's been flying 737s for this carrier for the better part of two decades.
"So let me get this straight
Speed trim looks like MCAS activation. But I’m to ignore that
Fast trim looks like MCAS but I ignore that
Fast trim runway looks like MCAS but is deactivated by yoke, electric, and stab cutouts
Slow trim runaway could be mistaken for MCAS but is deactivated by yoke, electric, and stab cutouts
MCAS, when finally noticed can NOT be overridden by the yoke, takes 9 sec to go to the stops, and have to activate the cutouts while fighting the trim, opposing it with pilot activated electric slow mode trim, and increasing yoke forces. All this after having to go they the above scenarios in your head to determine what is happening. Yea. Sounds like a great plan"
So, although I will wait and see what comes out in the accident reports, my thinking right now is that there is going to be a lot of links in error chain where this accident could have prevented, but, the first links where these two accidents started was in the boardroom and engineering floor at Boeing and in the back offices of the FAA. That's where this accident should have been prevented. Not at 1000' AGL over Ethiopia with an experienced, but under trained Captain and new FO fighting an airplane with the stick shaker activated, alarms sounding, and unreliable airspeed and AOA indications.