Pyrpolizer wrote:Kikapu wrote:Did Boeing tried too hard to add a "safety feature" into the B-737 max planes that would prevent another Air France 447 disaster, but instead, have become anything but?
AF447 flying from Brazil to France crashed into the Pacific Ocean with it's nose up attitude as the pilots got totally confused as the instruments stopped working correctly for a while due to the Pitot tubes freezing up, because the automated warning system commanded the pilot to "pull up, pull up", which the pilot complied, but the plane crashed anyway killing all aboard. What the pilot in command didn't realize, was that the plane's nose was up, but too much, which with full power, it was still coming down as the wings stalled and it was coming down in an almost 45% angle facing up while mushing through the air forward. Being in complete darkness, the pilots lost all awareness what the plane was doing, other than it was going to crash.
All pilots learn one thing very early in their training, that when the wings are stalling, is to add power and/or bring the nose of the aircraft down regardless how close one is to the ground, because maintaining status quo will result in a crash. The AF447 pilot only added power, but did not put the nose down. So, did Boeing wanted to make the plane put the nose down automatically if the pilots got confused? Sounds like a good safety feature to have, but it appears, the software is not done properly as it is normal for planes to have a high nose up attitude during takeoff and the need of the automated action by the plane to bring the nose down at such early in the flight wouldn't be necessary. But it seem, it is the reason of the two crashes of the B-737 Max's crashes so far as the pilots were not able to pull the nose up because the computer wouldn't allow it.
Shhhh... Paphitis will freak out.
Why would I freak out? Kikapu is asking some great questions.
I got no problem with Kikapu's post. What is evident to me once again is the fact that the media are creating a huge media storm against Boeing that is unwarranted. And most of what they are saying is nonsense. People take the bait and there is even talks of conspiracy and negligence. It's beyond Boeing's capability to eliminate stupidity when operating their aircraft. Their aircraft was not operated compliantly as Boeing intended it to be operated and this resulted in a crash. Also bear in mind that the B737 MAXI and its MCAS is certified in all jurisdictions around the world (America's, EU, Australia you name it) and in order to do this, the system has been tested for thousands of hours.
So far, the media are saying that because there were 2 crashes quite possibly with MCAS as a contributing factor, that it must be Boeing's fault and that the entire fleet should be grounded. This is NOT the case. The accident was caused because 2 pilots stalled the aircraft. This is the primary cause. This is a situation that is completely avoidable by proficient and experienced pilots. Pilots should never rely on Stall Avoidance. To me, this is unacceptable. Also, the grounding is precautionary. The MCAS is just a safety feature, not a replacement to good Airmanship.
Anyway it will all come out in due course. The B737 MAXI will also be flying within the next few days as well.
Rest assured, Boeing knows what it is doing. The B737 is probably the best built aircraft and most successful aircraft ever built.
This technology isn't new. Stall Avoidance Systems have been in commercial aircraft over 5700KGs in the Regular Public Transport category of operations since WW2.
Things like Stick Shakers and Stick Pushers are one such safety feature. The Maneuvering Characteristics Augmentation System (MCAS) fitted on the B737 MAXI is just a Fly By Wire electronic version of the more mechanical Stick Pusher and Stick Shaker system but a side affect is that the pilots have less control. That is the issue here. A problem that can be easily fixed with an upgrade to the software and better pilot training. There is definitely a training issue element in the Ethiopian Airlines Crash.
Stall Avoidance Systems are also not only triggered by a high Angle of Attack. It's also triggered by
low airspeed. For instance, the most dangerous phase for Stall Avoidance is actually on the LANDING with a lower Angle of Attack than on the Take OFF with a high Angle of Attack. Airspeed on Rotation is about the same as Landing Airspeed at the Touch Down Markers (there is a small variance) but the aircraft accelerates fast to 180 knots to the acceleration altitude where the attitude is lowered to accelerate to 220 knots in the second segment of climb where it is safe from ground obstacles. This acceleration is achieved by lowering the attitude or Angle of Attack. Also, the power is reduced from Take of Power to Climb Power (an arbitrary setting dependent on Outside Air Temperature and Weight in order to achieve the right performance in the second segment, a legislated performance criteria that is in The Civil Aviation Orders Section 20.7.1b for high capacity RPT aircraft.
Boeing and Airbus have been building compliant aircraft to meet these requirements for decades. The issue is in the software and in pilot training. Sadly in Aviation, new technology quite often results in loss of life until the authorities can re-calibrate because its uncharted territory which will ultimately make aviation safer when everyone is across this capability. What I believe occurred is that the airline did not keep up with this technology in educating its pilots. There were hundreds of B737 MAXI aircraft flying around the world without incident.
Now, I stated that the most dangerous phase is landing. You have a lower Angle of Attack but a very low airspeed that is 1.2 Vstall. So you got a 20% margin above the stall on short finals below 500FT Above the Ground on an approach meeting the Stable Approach Criteria - Rate of Decent below 1000 Feet per minute, wings level, on the centreline, on the glide-slope and in tolerance (half scale deflection) and all landing checks complete. So you got your Vref which is what you should be as the aircraft touches down on the Markers. Vref is 1.2 Vstall.
When the airspeed reduces by 7 knots below Vstall - the Stall Avoidance activates. This is the start. Pilot intervention is easy. Plane is easily recovered.
When the airspeed reduces further by another 7 knots, a force is applied to the Control Column to lower the nose and increase airspeed. Imagine this on Short Final. This is the most likely time. This is a lot harder for pilot intervention, but the plane should NEVER get there and if it does the pilots have failed in their duties. You apply max power to accelerate the aircraft and execute a missed approach Go Around, where you rotate from a low Angle of Attack to a Climb Angle of Attack. This is a serious safety occurrence resulting in a safety Report.
The stall is entered by a further 7 knot reduction - aircraft stalls. Everyone dies.
This is what the MCAS is.
The problem with this accident I hate to say is mostly pilot error. The pilots should have never found themselves in this position.
I have had a SAS event (Stall Avoidance Event) only once in the last 12 months (in about 800 hours of flying) and that was a minor 7 knot deviation caused by wind shear when I was landing at Sydney Runway 34R on a stormy day. These events are rare because we are trained to follow procedures and maintain our speeds. Also, we add additives for gusty conditions and wind shear. In other words we add 50% of the wind gust component to our Vref in order to add an additional safety margin.