Failed Avionics a Possible Cause of BA038 Crash
Muhammar writes "As you may have heard by now, both engines of the Boeing 777 aircraft flight BA038 suddenly cut off without warning at very low altitude and low speed during autopilot-assisted landing at Heathrow. A prompt reaction of the pilots prevented the stall and saved all lives aboard. The crash landing short of the runway tore off the landing gear on impact, and the fuselage plowed a long, deep gouge in the grass. With the investigation ongoing, the available information points to an electronic control problem as the most likely cause of the sudden engine power loss."
A bit of FUD here I think - unless I read TFA wrong, the entire thing is under investigation and no one is saying anything for at least a month. The autopilot apparently sensed the need for more thrust and warned the pilots of this. It might be premature to say that a software problem is the likely cause of failure...
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The pilots then manually increased throttle - to no avail.
For both engines to malfunction like this at the same time greatly seems to point to a fuel delivery problem.
This does not necessarily mean "running out of gas" - as a plane like this has multiple tanks, valves and pumps, all of which can be configured multiple different ways - which change during the flight.
A simplistic example: they could have been running both engines off one tank - which went dry - though another was full - or both engines were being fed from a common fuel pump which failed, etc. These things *shouldn't* happen - but the investigation will tell...
What I've read is that the pilots observed a relatively gradual loss of power symmetrically on both engines. This tells me that I can rule out engine problems with FADEC and fuel. It all points to the auto-throttle. Autopilot tells where it wants the plane to go and autothrottle calculates how much throttle is needed. It then commands both engines FADECs via the bus system which is doubly redundant. What I'm thinking is that auto-throttle is supposed to be backed up, bypassed by a manual direct control to the engine FADECs from the cockpit throttle control?
Any B777 avionics mechanics around - I only know military jets...
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Let's just wait for the official forensics rather than patched together rumours shall we?
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I believe what they meant, was that the pilots realized that things were going wrong, and the "normal" reaction would be to add thrust. When they realized that they couldn't add thrust, that this would result in loosing airspeed, entering a stall, and crashing
So they realized that an alternative was to lower their angle-of-attack, preventing the stall, and maintaining a bit of airspeed. This would have the unfortunate side affect of landing well-short of the runway (and perhaps airport) and destroying the aircraft - but given the information available - was a bad - but the best alternative
So they implicitly decided the best course of action was to glide the airplane and ditch it in a field - not a decision that would have exactly won them any praise had they read the situation wrong - but it saved everyone
If a cell phone can do this much damage, why the hell am I allowed to bring one (several even) on a plane?! These days, a swiss army knife will maybe get you as far as row 6 before people dogpile you, and they are confiscated. But a plane has easily 50 cell phones on it at any given time. If the only thing between me and engine failure are passengers dutifully following crew member instructions, then we are all screwed. So I am going to respectfully suggest that you are mistaken, because the alternative seems ludicrous.
Trans-Atlantic flights are often 90 minutes of flying time from a suitable runway. Trans-Pacific flights can be 3 hours or more of flying time from a suitable runway. Needless to say, airlines cannot glide with no power for hours. Air Canada Flight 143 (see http://www.wadenelson.com/gimli.html) was estimated to have a glide ratio of 11:1 with both engines windmilling. So from 40,000 ft, the maximum glide distance would have been about 100km. Sink rate was estimated at 2000 ft/sec meaning with all engines out, you will be visiting some destination at sea level within about 20 minutes.