Comment by lazystar
2 days ago
still, it at least shows that there's been issues with the locking mechanism in the past. inadvertently bumping something that was assumed to be locked is a simpler theory; i find it hard to believe that a murder suicider would take this route, when the china nosedive option is easier, faster, and has a higher chance of success.
The preliminary report says the switches were triggered a second apart, so it would have to have been faulty switches and two inadvertent bumps. That seems unlikely to me.
Within a second apart. If I read the report right. The time resolution of the recorder?
And yes, it does sound like it was probably intentional. I would still like to see an engineering review of the switch system. Are they normally open or normally closed, In the end the switch instructs the FADEC to cut the fuel, but where does the wiring go in the meantime? what software is in the path? would the repair done before the flight be in that area?(pilot defect report for message STABS POS XCDR), and perhaps compromised the wires?
Cutting fuel just after takeoff leaves almost zero time for the other pilot to recover.
it only guarantees an accident it doesn’t guarantee death of the pilot, at such low altitude and speed anyone can survive as the one passenger did .
Why would anyone risk potentially surviving a sabotage like that ?
A fully fueled plane crashing in takeoff guarantees a huge fire.
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It's interesting to try to imagine a device that would prevent that, without causing more issues.
My preliminary idea is a "fuel bladder" for take-off that inflates with enough fuel to get the plane to a recoverable altitude, maybe a few thousand feet?
I think engine fires are still more common than suicidal pilots and inadvertant fuel shutoff activations.
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Or you simply interlock the engine cutoff with the thrust lever position, any position other than idle prevents shutdown. This all goes through the flight computers already.
If there’s a fire or similar problem the fire handles will cut off fuel without the normal shutdown procedure, but the normal switches only need to be used at idle thrust.
I wonder if Airbus has this logic, since their philosophy is to override the pilot commands if they’d endanger the aircraft (which has its own issues of course) where’s Boeing will alert the pilots and still perform the action. I don’t have access to that information.
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> My preliminary idea is a "fuel bladder" for take-off that inflates
Will the bladder be marketed by Kramerica Industries?