767jetz
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- Aug 20, 2002
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RDU Jetblast said:If it is brake by wire, and power was lost just prior to touchdown, there might not have been time for the back up systems to kick in while the computers were re-booting.
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It doesn't work that way. Redundant systems take over in milliseconds. There are no computers to re-boot.
More likely, one contributing cause could be a function of the autothrottle system called "Managed Speed." The airplane is flown in managed speed during an approach, and the computer uses a complicated logarithm based on weight, density altitude, wind, ground speed, etc. to calculate an approach speed. It is a dynamic fucntion that is constantly changing. It looks at something called "Mini-Groundspeed" (minimum ground speed) in order to preserve energy in the event of windshear that shears from a head wind to a tail wind. It is an incredible tool for flying out of a windshear event if one is encountered in the air, like the one that brought down the Delta L1011 20 years ago. I have flown airbus simulators through windshear events with and with out Managed Speed, and I can tell you first hand that it works perfectly as designed.
The draw back is that if you are flying into a strong head wind, due to Mini-Groundspeed the approach speed can be excessively high, making the landing roll longer. In this case it is often better to disengage managed speed on short final and pick a compromise speed. Add to that a long landing, heavy weight, and a wet runway, and it's not hard to see how an over-run is possible.
RDU Jetblast said:Just like when the tail fell off of that AA flight in NY, they said something to the effect that the pilot shouldn't have applied so much pressure to the rudder. Does anyone else see a pattern?
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I agree that aircraft manufacturers will always try to claim pilot error in order to avoid accountabilility. In the case of AA, the problem was NOT the amount of rudder used. It was the reversal of control inputs from full left to full right, several times. This technique is appropriate in small aircraft and even military and aerobatic airplanes. But no transport catagory airplane is designed to withstand that kind of structural stress. Full rudder input is OK. Full deflection one side to the other is not.
They should have known that.
But in the pilot's defense, there was a lack of information from Airbus on this matter, a lack of specific training from AA, and a design flaw that allowed small pilot inputs to equal large control movements with little feedback to the pilot.